View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 17526U 87017B 22221.63719870 .00000138 00000-0 12369-3 0 9990
2 17526 82.8988 75.5344 0041697 102.0358 258.5477 13.76937406764595
Epoch (UTC): | 09 August 2022 15:17:33 |
Eccentricity: | 0.0041697 |
inclination: | 82.8988° |
perigee height: | 944 km |
apogee height: | 1005 km |
right ascension of ascending node: | 75.5344° |
argument of perigee: | 102.0358° |
revolutions per day: | 13.76937406 |
mean anomaly at epoch: | 258.5477° |
orbit number at epoch: | 76459 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|